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2835-00-116-5506
Nonaircraft Gas Turbine Engine Turbine Rotor Blade
2835001165506 001165506 1-100-428-20
An item mounted on a DISK, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, NONAIRCRAFT. View more Nonaircraft Gas Turbine Engine Turbine Rotor Blade
January 2023
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Restrictions 2835-00-116-5506
2835-00-116-5506 is a Nonaircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 2835-00-116-5506
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2835-00-116-5506
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
Approved Sources 2835-00-116-5506
- Part Number
- Manufacturer
- Status
- 1-100-428-20
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2835-00-116-5506
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Special Features [FEAT]
- Nickle Alloy, M3602 Fscm 91547, Rockwell C Scale 32 Min,
NATO Stock Numbers Related to 2835-00-116-5506
Freight Information 2835-00-116-5506
2835-00-116-5506 has freight characteristics.. 2835-00-116-5506 has a variance between NMFC and UFC when transported by rail and the description should be consulted.